Boldface Ops Limits Flashcards

1
Q

Engine Fire During Ground OperationS

A

THROTTLES - CUTOFF

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2
Q

Engine Fire During Flight

If engine fire switchlight remains illuminated, L or R FIRE DET FAIL illuminates, fire warning test fails, or fire conditions persist:

A

THROTTLE IDLE

THROTTLE - CUTOFF
ENGINE FIRE SWITCH - PUSH
BOTTLE ARMED SWITCH - PUSH

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3
Q

Smoke Or Fumes In Aircraft

A

OXYGEN MASKS - DON / 100%

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4
Q

Pitch Trim/Roll Trim/Rudder Trim Runaway

A

TRIM INT & A/P DISENGAGE SWITCH - PUSH AND HOLD

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5
Q

Low Cabin Pressure

A

OXYGEN MASKS - DON / 100%

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6
Q

Engine:
Thrust Setting: Takeoff
Time Limit (Minutes):

A

5 (1)

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7
Q

Engine:
Thrust Setting: Maximum Continuous
Time Limit (Minutes):

A

Continuous

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8
Q

Engine:
Thrust Setting: Idle
Time Limit (Minutes):

A

Continuous

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9
Q

Engine:
Thrust Setting: Takeoff
Maximum Observed ITT degrees C:

A

700

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10
Q

Engine:
Thrust Setting: Maximum Continuous
Maximum Observed ITT degrees C:

A

680

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11
Q

Engine:
Thrust Setting: Idle
Maximum Observed ITT degrees C:

A

580

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12
Q

Engine:
Thrust Setting: Starting (4)
Maximum Observed ITT degrees C:

A

550 - 600 4 SEC
600 - 700 2 SEC
700 - 720 1 SEC

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13
Q

Engine:
Thrust Setting: Transient
Maximum Observed ITT degrees C:

A

(720 2 SEC Max)

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14
Q

Engine:
Thrust Setting: Takeoff
N2%:

A

96

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15
Q

Engine:
Thrust Setting: Miximum Continuous
N2%:

A

96

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16
Q

Engine:
Thrust Setting: Idle
N2%:

A

52 (Min)

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17
Q

Engine:
Thrust Setting: Transient
N2%:

A

96

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18
Q

Engine:
Thrust Setting: Takeoff
N1%:

A

104

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19
Q

Engine:
Thrust Setting: Maximum Continuous
N1%:

A

104

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20
Q

Engine:
Thrust Setting: Transient
N1%:

A

106

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21
Q

Engine:
Thrust Setting: Takeoff
Oil Pressure (2) PSI:

A

60 to 83

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22
Q

Engine:
Thrust Setting: Maximum Continuous
Oil Pressure (2) PSI:

A

60 to 83

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23
Q

Engine:
Thrust Setting: Idle
Oil Pressure (2) PSI:

A

40 (Min)

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24
Q

Engine:
Thrust Setting: Transient
Oil Pressure (2) PSI:

A

95 for 90 SEC

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25
Engine: Thrust Setting: Takeoff OilTemperature (degrees C):
10 to 121
26
Engine: Thrust Setting: Maximum Continuous OilTemperature (degrees C):
10 to 121
27
Engine: Thrust Setting: Idle OilTemperature (degrees C):
-40 to 121
28
Engine: Thrust Setting: Starting OilTemperature (degrees C):
-40 (Min)
29
Engine: Thrust Setting: Transient OilTemperature (degrees C):
135 (Max) (15 MIN Max)
30
(2) Normal Flight: Normal oil pressure is ___ to ___ PSI at N2 speeds above ___%. Oil pressure below ___ PSIis undesirable and should be tolerated only for the safe recovery of the flight, preferably at reduced power setting. Oil Pressure below ___ PSI is unsafe.
``` 60 83 60 60 40 ```
31
(3) Under cold starting conditions, oil pressure between ___ PSI and ___ PSI is limited to ___ seconds.
83 95 90
32
(4) The ITT during ground starts should normally not exceed ___ degrees C.
550
33
Normal hydraulic pressure ___ to ___ PSI
1350 to 1550
34
Normal nitrogen pressure ___ to ___ PSI
1350 to 1650
35
Normal oxygen pressure ___ to ___ PSI
1600 to 1850
36
Min battery voltage for battery start ___ volts
22
37
Max gen load prior to starting second engine ___ amps
150
38
Motoring of the starter is limited to: First, ___ seconds then ___ minutes cooling. Second, ___ seconds then ___ minutes cooling. Third, ___ seconds then ___ minutes cooling.
30 5 30 15 30 60
39
Emergency Fuel / Minimum Fuel ___ lbs / ___ lbs
300 / 500
40
Maximum Fuel Imbalance - T.O./Touch & Go ___ lbs
100
41
Max Fuel Imbalance - Flight ___ lbs
300
42
Max Fuel Imbalance - Landing ___ lbs
300
43
Fuel crossfeed with 2 engines operating is limited to level flight with less than ___ lbs of fuel remains in the wing tank supplying fuel.
600
44
Max Ramp Weight ___ lbs
16,300
45
Max Takeoff Weight ___ lbs
16,100
46
Max Landing Wieght ___ lbs
15,700
47
Extend flaps to 10 degrees ___ KIAS
200
48
Extend flaps >10 degrees ___ KIAS
170
49
Flaps extended > 10 degrees ___ KIAS
165
50
Aircraft if limited to ___ KIAS or ___ MACH, whichever is less
330 .78
51
Landing Gear/Lights ___ KIAS / FL ___
200 200
52
Wipers ___ KIAS
200
53
Tire ___ Knots GS
165
54
Max Tailwind ___ Knots
10
55
Max Crosswind (Dry)___ Knots
25
56
Max Crosswind (Wet)___ Knots
15
57
Max Crosswind (Icy)___ Knots
10
58
Max Operating Altitude FL ___
410
59
Yaw Damper required operable for flight above FL ___
280
60
Do not use autopilot below ___ FT AGL
200
61
Except for preflight checks and landing rollout, do not operate anti-ice systems during ground operations at temperatures above ___ degrees C OAT/SAT
10
62
Do not operate surface anti-ice systems in flight at ram air temperatures above ___ degrees C.
10
63
To ensure proper wing anti-ice operations, the throttles must be kept at ___% N2 minimum.
70